IMI 834钛合金的热变形行为及有限元模拟OA
Hot Deformation Behavior and Finite Element Simulation of IMI 834 Titanium Alloy
IMI 834钛合金是一种具有优异综合性能的近α型钛合金,是航空发动机用耐550~600 ℃高温钛合金,在航空航天领域具有广泛的应用前景.然而IMI 834合金由于α+β两相区狭窄,导致合金锻造成型窗口小,因此合金组织性能对锻造工艺参数敏感.但目前针对IMI 834合金在高温变形过程中的组织演化机制尚缺乏系统研究.因此,本研究以IMI 834钛合金为研究对象,通过有限元模拟结合等温单向压缩实验,系统研究了不同变形温度(990、1 000和1 010 ℃)下合金的显微组织与织构的演变规律.实验采用直径为100mm 的圆柱试样,在50%变形量和3mm/s下压速率条件下进行单向热压缩.有限元模拟表明,在不同温度下,试样应变分布基本一致,应变梯度主要存在于外表层与心部之间,温度差异主要存在于心部与上下端面之间.这一应变和温度分布特征与实验观察到的组织差异具有明确对应关系:心部与外表层组织之间的显著差异,可归因于应变梯度所引发的不均匀变形,以及温度分布差异所导致的动态再结晶行为变化共同作用的结果.对压缩后样品不同区域的组织进行表征,结果表明,随着温度升高,初生α相含量逐渐减少,球化程度增加,试样从以动态回复为主逐渐转变为动态再结晶为主导,织构强度先增后减,组织均匀性提高.
IMI 834 titanium alloy is a near-alpha titanium alloy known for its excellent comprehensive properties.It serves as a high-temperature titanium alloy capable of withstanding temperatures between 550℃ and 600℃,making it suitable for use in aeroengines and offering broad application prospects in the aerospace field.However,owing to its narrow α+βtwo-phase region,the IMI 834 alloy has a limited forging process window,which results in a high sensitivity of its microstructure and properties to the forging parameters.Nevertheless,systematic studies on the evolution mechanisms of the microstructure and texture of IMI 834 alloys during high-temperature deformation are still lacking.Therefore,the evolution of the microstructure and texture of IMI 834 titanium alloys was systematically investigated at different deformation temperatures(990,1 000 and 1 010℃)through finite element simulations combined with isothermal unidirectional compression experiments.Cylindrical samples with a diameter of 100 mm were subjected to unidirectional hot compression under conditions of 50%deformation and a strain rate of 3 mm/s.Finite element simulations reveal that the strain distribution across the samples remained largely consistent at different temperatures,with strain gradients primarily observed between the outer surface and the core,whereas temperature variations exist between the core and the upper/lower end surfaces.These strain and temperature distribution characteristics clearly correspond to the microstructural differences observed experimentally:the significant distinction between the core and surface-layer microstructures can be attributed to the combined effects of nonuniform deformation caused by strain gradients and variations in dynamic recrystallization behavior resulting from temperature distribution differences.Microstructural characterization of different regions of the compressed samples revealed that as the temperature increased,the content of the primary α phase gradually decreased,spheroidization became more pronounced,and the dominant deformation mechanism shifted from dynamic recovery to dynamic recrystallization.The texture intensity initially increased but then decreased,whereas the microstructural homogeneity improved.
杨草;刘浪;张林嘉;景春红;唐斌
西北工业大学材料学院,陕西西安 710072||中国航发贵州黎阳航空发动机有限公司,贵州贵阳 550014中国航发贵州黎阳航空发动机有限公司,贵州贵阳 550014西北工业大学材料学院,陕西西安 710072||海装广州局驻贵阳地区军事代表室,贵州贵阳 550000西北工业大学材料学院,陕西西安 710072||中国第二重型机械集团德阳万航模锻有限责任公司,四川德阳 618000西北工业大学材料学院,陕西西安 710072
矿业与冶金
单向压缩有限元模拟动态再结晶织构
unidirectional compressionfinite element simulationdynamic recrystallizationtexture
《铸造技术》 2026 (5)
557-566,10
凝固技术全国重点实验室自主课题(2024-ZD-03)
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